Quasi-optimum three-axis attitude control law for minimum time of rigid body, noting gyroscopic cross axis coupling


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    Title :

    Quasi-optimum three-axis control of a space vehicle.


    Contributors:
    Friedland, B. (author) / Tavantzis, J. (author) / Thau, F. E. (author)

    Publication date :

    1967-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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